Citation: | LI Jin, ZHU Zi-qiang, WU Zong-cheng, et al. Influence of Grid Structure on the Euler Solution[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(2): 186-189. (in Chinese) |
[1] Benek J A, Buning P G, Steger J L. A 3-D chimera grid embedding technique. AIAA 85-1523,1985. [2]Li J, Zhu Z Q, Chen Z M, et al. The Euler solution of a 3D wing with aileron. In:Zhuang F G, Tang Y N, Zhao D G, eds. Proceeding of the Third International Conf of Fluid Mechanics. Beijing:Beijing Institute of Technology Press,1998. 286~292. [3]Chakrabartty S K, Dhanalakshmi K, Mathur J S. An introduction to Jumgrid—a multiblock grid generation code. PD CF 9709. India:National Aerospace Laboratories,1997. [4]Van Leer B. Flux-Vector Splitting for the Euler equations[J]. Lect Notes in Physics, 1982, 170:507~512. [5]Jameson A, Schnnidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time stepping schemes. AIAA 81-1259,1981. [6]Hess R W, Jr Cazier F W, Wynne E C. Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations. NASA TP 2594,1986. [7]Obayashi S, Guruswamy G P. Navier-Stokes computations for oscillating control surfaces. AIAA 92-4431,1992.
|